Xuezhi Wanga,b,c,*, Hanying Wanga,c, Ming Conga,b, Wenbo Fand and Na Yuane,*
aSchool of Mechatronics Engineering, Shenyang Aerospace University, Shenyang 110136, China
bAECC Shenyang Liming Aero-Engine Co., LTD, Shenyang 110043, China
cKey Laboratory of Rapid Development & Manufacturing Technology for Aircraft (Shenyang Aerospace University), Ministry of Education, Shenyang 110136, China
dTeaching and Research Support Center Army Artillery and Air Defense Forces Academy, Shenyang 110065, China
eSchool of Information and Control Engineering, Liaoning Petrochemical University, Fushun 113001, China
This article is an open access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/4.0) which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.
This Article2025; 26(6): 950-962
Published on Dec 31, 2025
Correspondence toaSchool of Mechatronics Engineering, Shenyang Aerospace University, Shenyang 110136, China
bAECC Shenyang Liming Aero-Engine Co., LTD, Shenyang 110043, China
cKey Laboratory of Rapid Development & Manufacturing Technology for Aircraft (Shenyang Aerospace University), Ministry of Education, Shenyang 110136, China
eSchool of Information and Control Engineering, Liaoning Petrochemical University, Fushun 113001, China
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